2015TC25 help
Last update: 2025-09-10 00:30 UTC
Epoch
Orbit properties
  • Epoch
  • Semimajor Axis
  • Eccentricity (e)
  • Inclination (i)
  • Long. of Ascending Node (Ω)
  • Arg. of Perihelion (ω)
  • Mean Anomaly (M)
  • Perihelion distance
  • Aphelion distance
  • Asc. Node-Earth Sep.
  • Desc. Node-Earth Sep.
  • MOID
  • Orbit Period
  • U parameter
Value
1-sigma variation
Unit
Epoch
Value
61000.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.028396
1-sigma variation
0.000001
Unit
Eccentricity (e)
Value
0.116229
1-sigma variation
1.614E-7
Unit
-
Inclination (i)
Value
3.7435
1-sigma variation
6.424E-6
Unit
Long. of Ascending Node (Ω)
Value
18.8519
1-sigma variation
4.094E-6
Unit
Arg. of Perihelion (ω)
Value
80.5704
1-sigma variation
4.874E-5
Unit
Mean Anomaly (M)
Value
181.41531
1-sigma variation
0.00239
Unit
Perihelion distance
Value
0.908867
1-sigma variation
Unit
Aphelion distance
Value
1.147926
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.002706
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.031328
1-sigma variation
Unit
MOID
Value
0.001527
1-sigma variation
Unit
Orbit Period
Value
380.9248
1-sigma variation
Unit
U parameter
Value
3.7
1-sigma variation
Unit
-
A1
Value
162127.65638
1-sigma variation
19365.45466
Unit
10-15au/days2
A2
Value
-4412.75154
1-sigma variation
2631.56000
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA1A2
a9.65336E-13-1.36247E-14-2.17677E-12-1.78123E-124.68650E-11-2.34872E-99.44570E-32.57052E-3
e-1.36247E-142.60577E-147.04330E-13-7.61286E-145.47175E-142.20081E-11-1.30780E-3-7.02616E-5
i-2.17677E-127.04330E-134.12661E-117.47322E-12-1.18345E-105.40493E-9-1.08127E-1-7.38882E-3
Ω-1.78123E-12-7.61286E-147.47322E-121.67609E-11-1.11866E-104.61775E-9-4.71922E-2-5.03913E-3
ω4.68650E-115.47175E-14-1.18345E-10-1.11866E-102.37535E-9-1.15300E-75.60664E-11.25527E-1
M-2.34872E-92.20081E-115.40493E-94.61775E-9-1.15300E-75.73119E-6-2.41207E1-6.26004E0
A19.44570E-3-1.30780E-3-1.08127E-1-4.71922E-25.60664E-1-2.41207E13.75021E82.95527E7
A22.57052E-3-7.02616E-5-7.38882E-3-5.03913E-31.25527E-1-6.26004E02.95527E76.92510E6
Date of computation: 2025-09-10 00:30 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: